Open Access
Issue
Mechanics & Industry
Volume 21, Number 5, 2020
Article Number 515
Number of page(s) 15
DOI https://doi.org/10.1051/meca/2020064
Published online 13 August 2020
  1. G.P. Sutton, O. Biblarz, Rocket propulsion elements, 7th edn. (John Wiley & Sons, New York, 2001) [Google Scholar]
  2. G.V.R. Rao, Exhaust nozzle contour for optimum thrust, Jet Propulsion 28, 377–382 (1958) [CrossRef] [Google Scholar]
  3. J.M. Farley, C.E. Campbell, Performance of several method of characteristics exhaust nozzles, NASA TN D293, 1960 [Google Scholar]
  4. B.M. Argrow, G. Emanuel, Comparison of minimum length nozzles, ASME J. Fluids Eng. 110, 283–288 (1988) [CrossRef] [Google Scholar]
  5. B.M. Argrow, G. Emanuel, Computational analysis of the transonic flow field of two-dimensional minimum length nozzles, AIAA-1989-1822, in 20th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Buffalo, NY, 1989, June 12–14 [Google Scholar]
  6. L.Z. Dumitrescu, Minimum length axisymmetric Laval nozzles, AIAA J. 13, 520–531 (1975) [Google Scholar]
  7. J.D. Anderson Jr., Modern compressible flow with historical perspective, 2nd edn. (McGraw-Hill Book Company, New York, USA, 1982) [Google Scholar]
  8. J.D. Anderson Jr., Fundamentals of aerodynamics, 2nd edn. (McGraw-Hill Book Company, New York, USA, 1988) [Google Scholar]
  9. T. Zebbiche, Z. Youbi, Effect of stagnation temperature on the supersonic flow parameters with application for air in nozzles, Aeronaut. J. 111, 31–40 (2007) [CrossRef] [Google Scholar]
  10. M. White, A.I. Sayma, C.N. Markides, Supersonic flow of non-ideal fluids in nozzles: An application of similitude theory and lessons for ORC turbine design and flexible use considering system performance, J. Phys.: Conf. Ser. 821 (2017) [CrossRef] [Google Scholar]
  11. A.P.S. Wheeler, J. Ong, The role of dense gas dynamics on organic Rankine cycle turbine performance, J. Eng. Gas Turb Power 135 (2013) [Google Scholar]
  12. A.C. Aldo, B.C. Argrow, Dense gas-flow in minimum length nozzles, J. Fluids Eng. 117, 270–276 (1995) [Google Scholar]
  13. M. Boun-jad, T. Zebbiche, A. Allali, High temperature gas effect on the Prandtl-Meyer function with application for supersonic nozzle design, Mech. Ind. 18, 219 (2017) [CrossRef] [Google Scholar]
  14. M. Boun-jad, T. Zebbiche, A. Allali, High temperature gas effect on the supersonic axisymmetric Minimum Length Nozzle design, Int. J. Eng. Tech. Res. 7 (2017) [Google Scholar]
  15. T. Edwards, Liquid fuels and propellants for aerospace propulsion, 1903–2003, J. Propul. Power 19, 1089–1105 (2003) [CrossRef] [Google Scholar]
  16. R. Amri, T. Rezoug, Numerical study of liquid propellants combustion for space applications, Acta Astronautica 69, 485–498 (2011) [Google Scholar]
  17. O. Abada, T. Zebbiche, A. Abdallah El-hirtsi, Three-dimensional supersonic minimum length nozzle design at high temperature for arbitrary exit cross section, Arab. J. Sci. Eng. 39, 7258–7879 (2014) [Google Scholar]
  18. T. Zebbiche, Rapid design method and new contours for a class of three dimensional supersonic nozzle of arbitrary exit cross section, Mech. Ind. 19, 403 (2018) [CrossRef] [Google Scholar]
  19. T. Zebbiche, Stagnation temperature effect on the supersonic axisymmetric minimum length nozzle design with application for air, Adv. Space Res. 48, 1656–1675 (2011) [Google Scholar]
  20. D.D. Esch, W. Siripong, A.R. Pike, NASA technical report on the thermodynamic properties in polymonial form for carbon hydrogen nitrogen and oxygen systems, Louisiana, USA, 1970 [Google Scholar]
  21. H. Kbab, M. Sellam, T. Hamitouche, S. Bergheul, L. Lagab, Design and performance evaluation of a dual bell nozzle, Acta Astron. 130, 52–59 (2017) [CrossRef] [Google Scholar]

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